Improving the mass efficiency of a composite launch vehicle head fairing with a sandwich structure

Author:

Kondratiev AndriiORCID

Publisher

Private Company Technology Center

Subject

Applied Mathematics,Electrical and Electronic Engineering,Management of Technology and Innovation,Industrial and Manufacturing Engineering,Computer Science Applications,Mechanical Engineering,Energy Engineering and Power Technology,Control and Systems Engineering

Reference37 articles.

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2. New satellite project Aerosol-UA: Remote sensing of aerosols in the terrestrial atmosphere;Milinevsky;Acta Astronautica,2016

3. Slyvyns’kyy, V., Gajdachuk, V., Gajdachuk, А., Slyvyns’ka, N. (2005). Weight optimization of honeycomb structures for space applications. 56th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law. doi: https://doi.org/10.2514/6.iac-05-c2.3.07

4. Slyvynskyi, V. I., Sanin, А. F., Kharchenko, М. Е., Kondratyev, А. V. (2014). Thermally and dimensionally stable structures of carbon-carbon laminated composites for space applications. Conference: 65th International Astronautical Congress. At Toronto, Canada.

5. Griffin, M. D., French, J. R. (2004). Space vehicle design. Reston. doi: https://doi.org/10.2514/4.862403

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